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Jameson RJJ-1 Gipsy Hawk : ウィキペディア英語版 | Jameson RJJ-1 Gipsy Hawk
The Jameson RJJ-1 Gipsy Hawk was a single-engine light aircraft intended to be homebuilt from plans. The prototype was designed and constructed in the U.S. by Richard Jameson in the late 1960s-early 1970s. ==Design and development==
The Gypsy Hawk was an all-metal low wing monoplane, constructed throughout from light alloy angle spars and frames under a light alloy skin. The wings and tailplane had constant chord and square tips. There was a fuel tank in the outer panel of each wing. The all-moving tail was set at the extreme rear fuselage and had external mass balances and an anti-servo tab. The fin and rudder were further forward, swept and with a fillet to lead the fin into the strongly sloping upper fuselage.〔 The fuselage was a light alloy semi-monocoque with a nose-mounted 65 hp (48 kW) Continental A65 flat-four engine driving a fixed pitch, two-blade propeller. The single-seat cockpit placed the pilot over the wing under a two-piece blown canopy. The Gypsy Hawk had a fixed, unfaired tricycle undercarriage.〔 Construction of the Gypsy Hawk began about 1968 and the first flight was in 1972.〔〔
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Jameson RJJ-1 Gipsy Hawk」の詳細全文を読む
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